BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual page 120

MASTER
ASSOCIATED
WARNING
ANNUNCIATOR
ANNUNCIATOR
BLEED
DUCT
CLOSED
DUCT
FAIL
FAIL
FLASHER
DUCT
FAIL
SENSOR
FAIL
OVHT
OVHT
ISOL
OPEN
FLASHER
STALL
PUSH
STALL
PROTECT
FAIL
ALT
COMP
FAIL
LH ENG
FIRE
PUSH
APU
FIRE
PUSH
OVHT
OVHT
NOSE
DOOR
OPEN
AP DISC
YD OFF
PARKING
BRAKE
ICE
ICE
LOP
CL-600-2B16 PILOT TRAINING MANUAL
Table 4-3. WARNING ANNUNCIATORS
CAUSE FOR ILLUMINATION
A leak is detected in the L/R 10th- or
14th-stage bleed-air manifold.
A leak is detected in the wing or
fuselage ducting.
An overheat is detected in a wing
leading edge.
The IAS is within 3% of the
aerodynamic stall.
The indicated computer channel
is unserviceable.
The altitude compensator is
selected off or has failed.
RH ENG
FIRE
PUSH
Indicated engine or APU has a fire.
The main landing gear bay
has an overheat.
The jet pipe/pylon has an overheat.
The nose gear doors are open.
Steady—The autopilot has been
manually disconnected
Flashing—The autopilot has
automatically disconnected
The parking brake is engaged.
Ice has been detected, but the
anti-icing systems for wing and
engines are not turned on.
The landing gear is in transit or is not
locked in the position selected, or the
LDG GEAR TEST button is pressed.
Engine oil pressure is low.
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
POWER
SOURCE
Dimming modules
Dimming modules
Dimming modules
Stall protect
computer power
supply
Dimming modules
Dimming modules
Fire detection unit
Overheat
detection unit
Dimming modules
Dimming modules
Ice detection units
Landing gear
control unit
Dimming modules
CL 601-3A/R 4-11
Lt é e
Lt d .